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ACwing FC firmware
STM32WB55: attitude IEKF, altitude Kalman filter, flight core, protocol v2
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#include <control_hooks.h>
Data Fields | |
| float | q [4] |
| IEKF attitude, body->world NWU, [w x y z]. | |
| float | dt |
| uint32_t | step |
Definition at line 25 of file control_hooks.h.
| float ctrl_att_in_t::q[4] |
IEKF attitude, body->world NWU, [w x y z].
Definition at line 26 of file control_hooks.h.
Referenced by on_acc_window().
| float ctrl_att_in_t::dt |
Definition at line 27 of file control_hooks.h.
Referenced by on_acc_window().
| uint32_t ctrl_att_in_t::step |
Definition at line 28 of file control_hooks.h.
Referenced by on_acc_window().